Search NASA⌕ Search

NASA NTRS · 19890028321

An explicit Runge-Kutta method for 3D turbulent incompressible flows

Abstract

A computer code has been developed to solve for the steady-state solution of the 3D incompressible Reynolds-averaged Navier-Stokes equations. The approach is based on the cell-center, central-difference, finite-volume formulation and an explicit one-step, multistage Runge-Kutta time-stepping scheme. The Baldwin-Lomax turbulence model is used. Techniques to accelerate the rate of convergence to a steady-state solution include the preconditioned method, the local time stepping, and the implicit residual smoothing. Improvements in computational efficiency have been demonstrated in several areas. This numerical procedure has been used to simulate the turbulent horseshoe vortex flow around an airfoil/flat-plate juncture.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Sung, Chao-Ho, Lin, Cheng-Wen, Hung, C. M.. 1988-01-01. An explicit Runge-Kutta method for 3D turbulent incompressible flows. https://ntrs.nasa.gov/citations/19890028321

Cite the original work for its findings. Save a collection to share your selection of sources.